Overall Trends
Total, fatal, and serious accidents in the selected range.
Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.
Fast key and full-text search with live filters, watches, and precise metadata.
Use quotes for exact phrase matches (for example "fuel selector valve").
Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.
Major cases, deep-report coverage, and investigation media across decades of NTSB history.
Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.
NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.
The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.
The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.
Frankfort, MI
THE PILOT OF A GLIDER TOW PLANE DESCENDED FOR LANDING AT HOME FIELD. THE ENGINE QUIT DUE TO FUEL EXHAUSTION AND THE AIRPLANE LANDED SHORT OF THE RUNWAY.
the pilot's failure to perform refueling.
On October 5, 1993, about 1600 eastern daylight time, a Piper PA-25-235 airplane, N6862Z, operated by Northwest Soaring Club experienced loss of engine power during descent and landed short of the runway at Frankfort, Michigan. The solo commercial pilot reported no injury. The airplane was substantially damaged. Visual meteorological conditions existed for the glider tow flight. The local flight originated about 1550 without a flight plan and operated under 14 CFR 91. The pilot reported the engine quit due to fuel exhaustion. No mechanical malfunction or failure was reported or found. When examined, the airplane contained less than a gallon of fuel and the fuel gage read empty. The pilot obtained a checkout in model the day before the accident.